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6360 Aluminum vs. EN 1.4578 Stainless Steel

6360 aluminum belongs to the aluminum alloys classification, while EN 1.4578 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is 6360 aluminum and the bottom bar is EN 1.4578 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 9.0 to 18
51
Fatigue Strength, MPa 31 to 67
200
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 76 to 130
400
Tensile Strength: Ultimate (UTS), MPa 120 to 220
550
Tensile Strength: Yield (Proof), MPa 57 to 170
200

Thermal Properties

Latent Heat of Fusion, J/g 400
290
Maximum Temperature: Mechanical, °C 160
930
Melting Completion (Liquidus), °C 640
1430
Melting Onset (Solidus), °C 630
1390
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 210
14
Thermal Expansion, µm/m-K 23
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 180
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
19
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.3
3.7
Embodied Energy, MJ/kg 150
51
Embodied Water, L/kg 1190
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 19
220
Resilience: Unit (Modulus of Resilience), kJ/m3 24 to 210
100
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 13 to 23
19
Strength to Weight: Bending, points 20 to 30
19
Thermal Diffusivity, mm2/s 86
3.9
Thermal Shock Resistance, points 5.5 to 9.9
12

Alloy Composition

Aluminum (Al), % 97.8 to 99.3
0
Carbon (C), % 0
0 to 0.040
Chromium (Cr), % 0 to 0.050
16.5 to 17.5
Copper (Cu), % 0 to 0.15
3.0 to 3.5
Iron (Fe), % 0.1 to 0.3
62.3 to 68.5
Magnesium (Mg), % 0.25 to 0.45
0
Manganese (Mn), % 0.020 to 0.15
0 to 2.0
Molybdenum (Mo), % 0
2.0 to 2.5
Nickel (Ni), % 0
10 to 11
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0.35 to 0.8
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0